Title:
ROTORCRAFT AND METHOD FOR CONTROLLING ORIENTATION THEREOF
Document Type and Number:
WIPO Patent Application WO/2021/250746
Kind Code:
A1
Abstract:
[Problem] To provide a flying object with which the falling body can be adjusted to a predetermined orientation and a parachute can be deployed more normally. [Solution] The present disclosure relates to a rotorcraft. The rotorcraft according to the present disclosure comprises a parachute mechanism that ejects a parachute in a predetermined direction and an orientation control means for adjusting the body to a specific orientation when the parachute is ejected. With this configuration, it is possible to reduce the damage, etc., caused when the flying object falls because the parachute can be deployed in a suitable orientation when deployed.
Inventors:
SUZUKI YOICHI (JP)
Application Number:
PCT/JP2020/022551
Publication Date:
December 16, 2021
Filing Date:
June 08, 2020
Export Citation:
Assignee:
AERONEXT INC (JP)
International Classes:
B64C39/02; B64D17/80; B64D45/04
Domestic Patent References:
| WO2019139073A1 | 2019-07-18 | |||
| WO2018066043A1 | 2018-04-12 |
Foreign References:
| JP2020059315A | 2020-04-16 |
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